págs. 385-390
Federated Kalman Filtering Via Formation of Relation Equations in Augmented State Space
V. A. Tupysev
págs. 391-398
Receding Horizon Control Lyapunov Function Approach to Suboptimal Regulation of Nonlinear Systems
J. Cloutier, M. Sznaier
págs. 399-405
Closed-Loop System Identification by Residual Whitening
C. H. Kuo, M. P. Schoen, S. Chinvorarat
págs. 406-411
págs. 412-419
págs. 420-429
págs. 430-437
págs. 438-444
Probabilistic Approach to Aircraft Performance Enhancement in Atmospheric Turbulence
A. Pieracci, G. Mengali
págs. 445-449
Gain-Scheduled Lateral Control of the F-14 Aircraft During Powered Approach Landing
I. Fialho, G. J. Balas, A. K. Packard
págs. 450-458
Adaptive Hysteresis Model for Model Reference Control with Actuator Hysteresis
A. Kurdila, G. Webb, D. Lagoudas
págs. 459-465
Evaluation of the Dynamic Environment of an Asterold: Applications to 433 Eros
Daniel J. Scheeres, B. G. Williams
págs. 466-475
Fuel-Optimal Planar Earth-Mars Trajectories Using Low-Thrust Exhaust-Modulated Propulsion
S. R. Vadali
págs. 476-482
Rapid Energy Dissipation in a Yo-Yo-Type Wire Boom Deployment System
P. M. Kintner, M. L. Psiaki
págs. 483-490
Optimal Vibration Control of Thin-Walled Anisotropic Cantilevers Exposed to Blast Loadings
S. Na, L. Librescu
págs. 491-500
Dynamics of a Variable-Mass, Flexible-Body System
A. K. Banerjee
págs. 501-508
Optimal Size and Location of Piezoelectric Actuator/Sensors: Practical Considerations
O. J. Aldraihem
págs. 509-515
Loop Shaping Design for Missile Autopilots: Controller Configurations and Weighting Filter Selection
P. A. Iglesias
págs. 516-525
Fast-Time Study of Airline-Influenced Arrival Sequencing and Scheduling
H. Erzberger, G. C. Carr
págs. 526-531
Accuracy of the Global Positioning System-Derived Acceleration Vector
M. L. Psiaki, P. M. Kintner, S. P. Powell
págs. 532-538
J. P. Norton, R. A. Best
págs. 539-546
págs. 547-553
págs. 554-555
Strategy for Deployment of Multiple Satellites for Collision-Free Relative Orbital Motion
R. V. Ramanan
págs. 556-557
Minimization of Vibration of Spacecraft Appendages During Shape Control Using Smart Structures
S. Kalaycioglu
págs. 558-560
Spacecraft Formation Flying: Dynamics and Control
J. M. Buffington, V. Kapila, A. G. Sparks
págs. 561-563
págs. 564-565
J. N. Huang, S. T. Lin
págs. 566-569
Application of a Dichotomic Basis Method to Performance Optimization of Supersonic Aircraft
A. V. Rao
págs. 570-572
Fuzzy-Logic-Based Closed-Loop Optimal Law for Homing Missiles Guidance
N. Rahbar, M. B. Menhaj
págs. 573-574
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